View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 64937U 26145.57165560 +.00000000 +00000-0 +16802-3 0 00005
2 64937 97.4539 9.4705 0002386 68.6169 291.5313 15.05655734 03
| Epoch (UTC): | 25 May 2026 13:43:11 |
| Eccentricity: | 0.0002386 |
| inclination: | 97.4539° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 9.4705° |
| argument of perigee: | 68.6169° |
| revolutions per day: | 15.05655734 |
| mean anomaly at epoch: | 291.5313° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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